EP 2098448 A1 20090909 - COMPOSITE PRESSURE BULKHEAD FOR AIRCRAFT
Title (en)
COMPOSITE PRESSURE BULKHEAD FOR AIRCRAFT
Title (de)
FLUGZEUGVERBUNDDRUCKSCHOTT
Title (fr)
CLOISON DE COMPRESSION FAITE D'UN MATÉRIAU COMPOSÉ POUR AÉRONEF
Publication
Application
Priority
ES 2006070186 W 20061129
Abstract (en)
The present invention relates to a curved rear pressure bulkhead (1) made of a composite material, comprising three layers: an outer layer (2) and an inner layer (3) symmetrical with one another, which are made of a fiber laminate, and the intermediate layer or core (4) made of a lightweight material. With such a sandwich-type shape, the resulting bulkhead (1) is able to withstand the bending loads coming from the strain and pressurization of the fuselage without having to increase its stiffness by means of using some type of stiffener. The bulkhead (1) comprises a ring (6) that is attached to the ends of the sandwich shape. This ring (6) is split into several parts (8) to facilitate the assembly of the bulkhead (1) made of composite material to the fuselage skin (5).
IPC 8 full level
B64C 1/10 (2006.01); B29C 70/08 (2006.01); B29C 70/34 (2006.01); B29C 70/54 (2006.01); B29C 70/86 (2006.01); B32B 37/10 (2006.01); B29K 105/04 (2006.01); B29L 31/30 (2006.01); B29L 31/60 (2006.01)
CPC (source: EP)
B29C 70/086 (2013.01); B29C 70/088 (2013.01); B29C 70/342 (2013.01); B29C 70/545 (2013.01); B29C 70/865 (2013.01); B64C 1/10 (2013.01); B29C 70/38 (2013.01); B29K 2105/04 (2013.01); B29L 2031/3076 (2013.01); B29L 2031/608 (2013.01); B32B 37/146 (2013.01); Y02T 50/40 (2013.01)
Designated contracting state (EPC)
AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HU IE IS IT LI LT LU LV MC NL PL PT RO SE SI SK TR
DOCDB simple family (publication)
EP 2098448 A1 20090909; EP 2098448 A4 20120808; WO 2008065214 A1 20080605
DOCDB simple family (application)
EP 06841793 A 20061129; ES 2006070186 W 20061129